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Mathematical Model and Computational Research of Combustion Chamber Wall Thermal State for Gaseous-Propellant Oxygen-Methane Low-Thrust Rocket Engine on a Pulse Mode
| Authors: Vorozheeva O.A., Yagodnikov D.A. | Published: 19.09.2013 |
| Published in issue: #7(640)/2013 | |
| Category: Calculation and Design of Machinery | |
| Keywords: low-thrust rocket engine, gaseous oxygen and methane, combust ion chamber, mathematical modeling, pulse mode, thermal state |